Project Title

AESOP-lite: Anti-Electron Sub-Orbital Payload – Low Energy

Summary

Event Number:
A-148-M
NSF / NASA Agreement

Program Manager:
Dr. Vladimir Papitashvili

ASC POC/Implementer:
John Rand / Kaija Webster / Chad Naughton

Principal Investigator(s)

Dr. John M Clem
clem@bartol.udel.edu
University of Delaware
Physics and Astronomy

Project Web Site:
https://sites.udel.edu/aesoplite/

Location

Supporting Stations: McMurdo Station
Research Locations: McMurdo LDB Site

Description

AESOP-lite's (Anti-Electron Sub-Orbital Payload- low energy) science goal is to explore the source of the negative spectral index of low energy cosmic ray electrons (20-100MeV). To accomplish this objective we will attack the problem from two fronts. First, we propose to measure electrons in the energy range of 20MeV to 300MeV with the AESOP-lite instrument on a high altitude balloon >140kft. This data will provide a clean, calibrated reference at 1AU to be compared with Voyager electron observations from interstellar space. Voyager I and II are currently returning electron spectra roughly within this energy range (<160MeV). Second, we plan to simultaneously measure the positron fraction in the electron flux within this low energy regime using the same instrument. Positron abundances in this energy range should be highly diagnostic of the particle origin. The primary science objective is to make a definitive determination of the cosmic electron and positron energy spectrum from 20MeV to above 500MeV.

Field Season Overview

Six participants will deploy in the 2022-23 season. In preparation of the balloon flight, the AESOP-lite payload will be assembled, evaluated for functionality and calibrated. This includes the integration of CSBF's flight equipment with the payload and a final compatibility test while hanging from the launch vehicle. A 400ft^2 assembly area with an 1/2 ton overhead lift is needed to perform these operations including 5 x 120V 60Hz power outlets with a peak current 10amps for each outlet. Also internet service is necessary to communicate with Operation Control Center at CSBF. We request three static IPs. One of the detectors in the instrument, a Gas Cherenkov detector, uses C3F8 gas and may require refilling before flight. Consequently 10lbs of C3F8 is required in the field. In order to re-validate the flight O-ring and feed-thru gasket integrity, on the ground, the instrument flight shell is pressurize with Nitrogen gas to 14.7 psi over ambient over 48 hours. This procedure simulates the pressure differential expected at float. This test takes place in an empty Sea-container. Therefore, T-size bottom of Nitrogen is needed. AESOP-lite's goal is to be ready to launch early-December on a 60 million cubic foot balloon platform. Desired float altitude is 155k-feet. Duration goal is 80 hours at desired height or one full circumpolar rotation.

Deploying Team Members